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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
Authors: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利) ; Tian ZW(田中伟); Cui K(崔凯)
  Favorite | View/Download：106/0 | Submit date：2024/01/22
High-pressure capturing wing Subsonic Numerical simulation Wing dihedral Stability |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
 Adobe PDF(2608Kb) | Favorite | View/Download：283/123 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | Favorite | View/Download：302/116 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1961Kb) | Favorite | View/Download：304/115 | Submit date：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
Adobe PDF(3918Kb) | Favorite | View/Download：558/183 | Submit date：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇)
Adobe PDF(2032Kb) | Favorite | View/Download：338/106 | Submit date：2019/05/29
Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |
